View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00051U 60009C 21059.31790123 .00000032 00000-0 11314-2 0 9991
2 00051 47.2117 275.8436 0105050 203.2512 156.3502 12.18272097695282
Epoch (UTC): | 28 February 2021 07:37:46 |
Eccentricity: | 0.0105050 |
inclination: | 47.2117° |
perigee height: | 1516 km |
apogee height: | 1684 km |
right ascension of ascending node: | 275.8436° |
argument of perigee: | 203.2512° |
revolutions per day: | 12.18272097 |
mean anomaly at epoch: | 156.3502° |
orbit number at epoch: | 69528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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